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[null,"1.","Record Nr.",null,"UNINA990001300270403321"]
[null,null,"Autore",null,"Heffter, Lothar"]
[null,null,"Titolo",null,"Kurvenintegrale und Begrundung der Funktionentheorie / L. Heffter"]
[null,null,"Pubbl/distr/stampa",null,"Berlin : Springer-Verlag, 1955"]
[null,null,"Disciplina",null,"511.33"]
[null,null,"Locazione",null,"MA1"]
[null,null,"Collocazione",null,"3-E-20"]
[null,null,"Lingua di pubblicazione",null,"Inglese"]
[null,null,"Formato",null,"Materiale a stampa"]
[null,null,null,"Livello bibliografico","Monografia"]
[null,"2.","Record Nr.",null,"UNINA9910709981303321"]
[null,null,"Autore",null,"Wood Richard M."]
[null,null,"Titolo",null,"Experimental and theoretical study of the longitudinal aerodynamic characteristics of delta and double-delta wings at mach numbers of 1.60, 1.90, and 2.16 / / Richard M. Wood and Peter F. Covell"]
[null,null,"Pubbl/distr/stampa",null,"Washington, D.C. : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , July 1985"]
[null,null,"Descrizione fisica",null,"1 online resource (119 pages, 1 unnumbered page) : illustrations"]
[null,null,"Collana",null,"NASA/TP ; ; 2433"]
[null,null,"Soggetti",null,"Delta wings"]
[{"$nulls":4},"Supersonic airfoils"]
[{"$nulls":4},"Mach number"]
[{"$nulls":4},"Sweptback wings"]
[{"$nulls":4},"Supersonic flow"]
[null,null,"Lingua di pubblicazione",null,"Inglese"]
[null,null,"Formato",null,"Materiale a stampa"]
[null,null,null,"Livello bibliografico","Monografia"]
[null,null,null,"Note generali","\"July 1985.\""]
[null,null,null,"Nota di bibliografia","Includes bibliographical references (page 119)."]